教育经历

　　2003/09 - 2008/07，中国科学院力学研究所，流体力学，博士，导师姜宗林

　　1999/09 - 2003/07，中国科学技术大学，理论与应用力学，学士，导师韩肇元

工作经历

 　　2018/08–现在, 北京理工大学，ld体育官网，教授

　　2017/06 –2018/08，北京理工大学，ld体育官网，特别研究员

　　2011/12 – 2017/05，中国科学院力学研究所，高温气动国家重点实验室，副研

　　2010/08 - 2011/12，中国科学院力学研究所，高温气动国家重点实验室，助研

　　2008/10 - 2010/08，中国科学院物理研究所，博士后

主要研究领域

　　爆震物理与推进，空气动力学，多相燃烧与爆炸

获奖情况

　　2018年获国家自然科学基金委优秀青年科学基金

　　2016年获中国科学院杰出科技成就奖（集体奖）

　　2014年入选中国科学院青年创新促进会

社会兼职

　　《推进技术》编辑委员会  委员

　　中国力学学会   激波与激波管专业委员会  委员

　　中国力学学会   爆炸力学专业委员会计算爆炸力学专业组   成员

　　中国航空学会   燃烧与传热传质专业委员会  委员

　　中国工程热物理学会  新型热力循环专业委员会 委员

教学工作

　　本科生《火箭燃气动力学Ⅰ》《计算流体力学》

　　研究所《化学流体力学》

近年来主要发表论文

　　1. P. Yang, H. D. Ng, H. Teng. Numerical study of wedge-induced oblique detonations in unsteady flow. Journal of Fluid Mechanics, 2019, 876, 264-287.

　　2. C. Yan, H.H. Teng, X.C. Mi, H.D. Ng. The Effect of Chemical Reactivity on the Formation of Gaseous Oblique Detonation Waves. Aerospace 2019, 6(6), 62.

　　3. C. Tian, H. Teng, H. D. Ng, Numerical investigation of oblique detonation structure in hydrogen-oxygen mixtures with Ar dilution. FUEL, 2019, 252: 496 - 503.

　　4. Y. Zhang, Y. Fang, H.D. Ng, H. Teng.Numerical investigation on the initiation of oblique detonation waves in stoichiometric acetylene-oxygen mixtures with high argon dilution. Combust. Flame, 2019, 204: 391-396.

　　5. Y. Fang, Y. Zhang, X. Deng, H. Teng, Numerical study of wedge-induced oblique detonation in acetylene-oxygen- argon mixtures. Phys. Fluids, 2019, 31, 026198.

　　6. P. Yang, H. Teng, H. D. Ng, Z. Jiang,Instability of oblique detonation surface with a two-step induction-reaction kinetic model. Proc. Combust. Inst., 2019, 37: 3537-3544.

　　7. X. Deng, B. Xie, H. Teng, F. Xiao. High resolution multi-moment finite volume method for supersonic combustion on unstructured grids. Applied Mathematical Modelling, 2019 66: 404–423,

　　8. Y.N. Zhang, L. Zhou, J. Gong, H.D. Ng, H. Teng. Effects of activation energy on the instability of oblique detonation surfaces with a one-step chemistry model. Phys. Fluids, 2018, 30, 106110

　　9. X. Deng, B. Xie, F. Xiao, H. Teng. New accurate and efficient method for stiff detonation capturing. AIAA Journal, 2018, 56: 4024-4038.

　　10. Y. Zhang, P. Yang, H. Teng, Z. Jiang, H. Ng, C. Wen. Transition between different initiation structures of wedge-induced oblique detonations. AIAA Journal, 2018, 56: 4016-4023.

　　11. Y. Fang, Z. Hu, H. Teng. Numerical investigation of oblique detonations induced by a finite wedge in a stoichiometric hydrogen-air mixture. FUEL, 2018, 234: 502-507.

　　12. P. Yang, H. Teng, Z. Jiang, H. Ng. Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model. Combust. Flame, 2018, 193: 246-256.

　　13. Y. Fang, Z. Hu, H. Teng, Z. Jiang, H.D. Ng. Effects of inflow equivalence ratio inhomogeneity on oblique detonation initiation in hydrogen-air mixtures. Aerospace Science and Technology, 2017, 71: 256-263.

　　14. P. Yang, H. Ng, H. Teng, Z. Jiang. Initiation structure of oblique detonation waves behindconical shocks. Phys. Fluids, 2017, 29, 086104.

　　15. H. Teng, H. D. Ng, Z. Jiang. Initiation characteristics of wedge-induced oblique detonation wave in a stoichiometric hydrogen-air mixture. Proceedings of the combustion institute, 2017, 36(2): 2735-2742.

　　16. G. Xiang, C. Wang, H. Teng, Y. Yang, Z. Jiang. Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges. Acta MechanicaSinica, 2016,32(3): 362-368.

　　17. G. X. Xiang, C. Wang, H.H. Teng, Z. L Jiang. Investigations of Three-Dimensional Shock/Shock Interactions over Symmetrical Intersecting Wedges.AIAA Journal, 2016,54(5) :1472-1481.

　　18. H. Teng, H. D. Ng, K. Li, C. Luo, Z. Jiang. Evolution of cellular structure on oblique detonation surfaces. Combustion and Flame, 2015, 162: 470-477.

　　19. T. Wang, Y. Zhang, H. Teng, Z. Jiang, H. Ng. Numerical study of oblique detonation wave initiation in astoichiometric hydrogen-air mixture. Physics of Fluids, 2015, 27(9), 096101.

　　20. Z. Sun, H. Teng, F. Xiao. A Slope Constrained 4th Order Multi-Moment Finite Volume Method withWENO Limiter. Communications in Computational Physics 2015, 18(4): 901-930.

　　21.  H. H. Teng, Z. L. Jiang, H. D. Ng. Numerical study onunstable surfaces of oblique detonations. Journal of Fluid Mechanics, 2014, 744: 111-128.

　　22.  H. Teng,Y. Zhang, Z. Jiang. Numerical investigation on the induction zone structure of the oblique detonation waves. Computers & Fluids, 2014, 95: 127–131.

　　23. H. Teng, Z. Jiang. Effects of different product phases in aluminum dust detonation modeling. SCIENCE CHINA Physics, Mechanics & Astronomy, 2013,56 (11): 2178-2185.

　　24. H. Teng, Z. Jiang. Numerical simulation of one-dimensional Aluminum particle-air detonation with realistic heatcapacities. Combustion and Flame, 2013, 160: 463-472.

　　25. H. H. Teng, Z. L. Jiang. On the transition pattern of the oblique detonation structure. Journal of Fluid Mechanics, 2012, 713: 659-669.

　　26. Y. Yang ,H. Teng , Z. Jiang, K. Takayama. Numerical investigation on three-dimensional shock wavereflection over two perpendicularly intersecting wedges. Shock Waves ,2012, 22:151–159.

　　27. H. Teng, Z. Jiang. Instability criterion of one-dimensional detonation wave with three-step chain branching reaction model. Chin. Phys. Lett., 2011, 28, 8, 084704

　　28. H. Teng,T. Fujiwara,T. Hoshi, T. Sogabe, S.-L. Zhang, and S. Yamamoto. Efficient and accurate linear algebraic methods for large-scale electronic structurecalculations with nonorthogonal atomic orbitals.  Physical Review B, 2011, 83, 165103 .